EP2113042B2 - Nappe de spunbond pré-consolidé, composite non tissé comprenant cette nappe, procédé et système continu de production de ce composite - Google Patents

Nappe de spunbond pré-consolidé, composite non tissé comprenant cette nappe, procédé et système continu de production de ce composite Download PDF

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Publication number
EP2113042B2
EP2113042B2 EP08715834.1A EP08715834A EP2113042B2 EP 2113042 B2 EP2113042 B2 EP 2113042B2 EP 08715834 A EP08715834 A EP 08715834A EP 2113042 B2 EP2113042 B2 EP 2113042B2
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layer
spunbonded
bonding
composite nonwoven
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German (de)
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EP2113042A1 (fr
EP2113042B1 (fr
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Galliano Boscolo
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ALBIS INTERNATIONAL Srl
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ALBIS INTERNATIONAL Srl
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    • D—TEXTILES; PAPER
    • D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
    • D04H—MAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
    • D04H3/00—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length
    • D04H3/08—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating
    • D04H3/10—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating with bonds between yarns or filaments made mechanically
    • D04H3/11—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating with bonds between yarns or filaments made mechanically by fluid jet
    • D—TEXTILES; PAPER
    • D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
    • D04H—MAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
    • D04H13/00—Other non-woven fabrics
    • D—TEXTILES; PAPER
    • D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
    • D04H—MAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
    • D04H3/00—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length
    • D04H3/016—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the fineness
    • D—TEXTILES; PAPER
    • D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
    • D04H—MAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
    • D04H3/00—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length
    • D04H3/08—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating
    • D04H3/14—Non-woven fabrics formed wholly or mainly of yarns or like filamentary material of substantial length characterised by the method of strengthening or consolidating with bonds between thermoplastic yarns or filaments produced by welding
    • D—TEXTILES; PAPER
    • D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
    • D04H—MAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
    • D04H5/00—Non woven fabrics formed of mixtures of relatively short fibres and yarns or like filamentary material of substantial length
    • D04H5/02—Non woven fabrics formed of mixtures of relatively short fibres and yarns or like filamentary material of substantial length strengthened or consolidated by mechanical methods, e.g. needling
    • D04H5/03—Non woven fabrics formed of mixtures of relatively short fibres and yarns or like filamentary material of substantial length strengthened or consolidated by mechanical methods, e.g. needling by fluid jet
    • D—TEXTILES; PAPER
    • D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
    • D04H—MAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
    • D04H5/00—Non woven fabrics formed of mixtures of relatively short fibres and yarns or like filamentary material of substantial length
    • D04H5/06—Non woven fabrics formed of mixtures of relatively short fibres and yarns or like filamentary material of substantial length strengthened or consolidated by welding-together thermoplastic fibres, filaments, or yarns
    • D—TEXTILES; PAPER
    • D04—BRAIDING; LACE-MAKING; KNITTING; TRIMMINGS; NON-WOVEN FABRICS
    • D04H—MAKING TEXTILE FABRICS, e.g. FROM FIBRES OR FILAMENTARY MATERIAL; FABRICS MADE BY SUCH PROCESSES OR APPARATUS, e.g. FELTS, NON-WOVEN FABRICS; COTTON-WOOL; WADDING ; NON-WOVEN FABRICS FROM STAPLE FIBRES, FILAMENTS OR YARNS, BONDED WITH AT LEAST ONE WEB-LIKE MATERIAL DURING THEIR CONSOLIDATION
    • D04H5/00—Non woven fabrics formed of mixtures of relatively short fibres and yarns or like filamentary material of substantial length
    • D04H5/08—Non woven fabrics formed of mixtures of relatively short fibres and yarns or like filamentary material of substantial length characterised by the method of forming fleeces or layers, e.g. reorientation of fibres or yarns
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T442/00—Fabric [woven, knitted, or nonwoven textile or cloth, etc.]
    • Y10T442/60—Nonwoven fabric [i.e., nonwoven strand or fiber material]
    • Y10T442/681—Spun-bonded nonwoven fabric

Definitions

  • the present invention relates to a novel pre-consolidated spunbonded web, and to a composite nonwoven comprising several layers, one of said layer being the said pre-consolidated spunbonded web.
  • the invention also relates to a method and continuous system for producing said novel absorbent composite nonwoven.
  • One first preferred application of the invention is the manufacturing of hydroentangled composite nonwoven for absorbing liquids and comprising at least a pre-consolidated spunbonded layer and an absorbent pulp layer.
  • One second preferred application of the invention is the manufacturing of hydroentangled composite nonwoven comprising at least a pre-consolidated spunbonded layer and a carded layer.
  • Spunbonding is a well-know technology used in the field of nonwoven.
  • a Spunbonded web is produced by depositing extruded spun filaments onto a collecting belt in a uniform random manner. The spunbonded web is then pre-consolidated for example by thermo-bonding, i.e. by applying heat and pressure by means of heated rolls. The thermo-bonding partially melt and fuse the filaments together, and imparts strength and integrity to the web.
  • Pre-consolidated spunbonded webs are widely used in many types of composite nonwoven, and for example in SS, SSS, SMS, SPC, SPS, SC, SMC nonwoven [ S: Spunbonded layer ; P : Pulp Layer; C : Carded Layer; M : Meltblown layer].
  • SPC or SPS nonwovens are more especially used for absorbing liquids, in particular, but non only, in the hygienic industry.
  • SC nonwovens are also used for making, for example, top sheets of diapers and training pants.
  • the properties of the spunbonded layers influence the strike trough time of the top sheet.
  • Absorbent composite nonwoven are widely used in the prior art for absorbing liquids, especially, but not only, in the hygienic industry for making products such as, for example, diapers or sanitary napkins.
  • Absorbent composite nonwovens generally comprise at least two layers: a consolidated nonwoven carrier and an absorbent layer.
  • An absorbent material widely used for making the absorbent layer is a fibre material generally referred as "pulp", and made of or containing fibres from natural sources such as woody and non-woody plants.
  • Woody plants include, for example, deciduous and coniferous trees.
  • Non-woody plants include, for example, cotton, flax, esparto grass, milkweed, straw, jute hemp, and bagasse.
  • a satisfactory connection of an absorbent pulp layer to a nonwoven carrier is known, e.g. from US patent No 3, 560, 326 or PCT application WO92/080834 , specifically through hydraulic needling of the pulp fibres of the absorbent layer with the consolidated nonwoven carrier.
  • US patent No 6, 836, 937 discloses a new process that overcomes this problem of high pulp loss. This process consists essentially in inserting a thin intermediate meltblown layer between the nonwoven carrier and the absorbent pulp layer. This technical solution increases however the production costs, since it involves the manufacture of a supplementary layer between the nonwoven carrier and the absorbent pulp layer.
  • PCT applications WO 2004/092472 and WO 2006/010766 disclose a method for manufacturing a hydroentangled composite nonwoven comprising a spunbonded layer and a pulp layer. More particularly, it is recommended in these publications to spin splittable multicomponent polymers filaments for making the spunbonded layer. These splittable multicomponent polymers filaments are composed of microfilaments having a count between 0.1dtex and 0.9dtex, and the splittable filaments have a count between 1.7dtex and 2.2dtex. The splitting of the filaments is obtained during the hydroentanglement step of the spunbonded layer.
  • PCT application WO 01/53588 and US patent No 6,836,938 disclose a method for producing a composite nonwoven, in particular for the production of a hygienic product, said method comprising the following steps:
  • One objective of this publication is to reduce the pulp loss during hydrodynamic water needling, and for achieving this objective, it is recommended in this publication to make only a light bonding of the fibres of the spunbonded layer during the compaction and thermo-bonding step, in such a way that the pulp fibres enter into an internal bonding with the fibres of the spunbonded nonwoven fabric in the hydrodynamic water needling.
  • An objective of the invention is to propose a novel pre-consolidated spunbonded web, more especially, but not exclusively, a novel pre-consolidated spunbonded web that is suitable for making hydroentangled composite nonwovens, and more particularly SPC, SPS, or SC nonwovens.
  • Another objective of the invention is to propose a novel pre-consolidated spunbonded web having a low air permeability and good mechanical properties, in particular good tensile properties.
  • Another objective of the invention is to propose a novel hydroentangled absorbent composite nonwoven comprising at least a spunbonded layer and an absorbent pulp layer for absorbing liquids, and a process and continuous system for producing said novel composite nonwoven.
  • Another objective of the invention is to obtain a hydroentangled absorbent composite nonwoven exhibiting improved mechanical properties, in particular good tensile properties, and good abrasion resistance properties.
  • Another objective of the invention is to obtain a hydroentangled absorbent composite nonwoven exhibiting an improved softness.
  • Another objective of the invention is to reduce pulp losses during the manufacturing process of the composite, especially during the hydrodynamic water needling step of the layers of the composite.
  • a first object of the invention is thus a method of producing a pre-consolidated spunbonded web (A), as defined in independent claim 1. Said method comprises the steps of :
  • the spunbonded layer (A') formed in step (a) comprises bilobal continuous microfilaments having a diameter (DI) less than or equal to 15 ⁇ m, and in that the pre-consolidation step (b) of the spunbonded layer (A') is performed by means of a bonding pattern having bonding dots, the density (DD) of said bonding dots being higher than or equal to 90 dots/cm 2 .
  • a second object of the invention is a method of producing a hydroentangled composite nonwoven comprising at least two superposed layers, and as defined in independent claim 5. Said method comprises the following steps:
  • the second layer can be a carded layer or a spunbonded layer.
  • the second layer is a pulp layer, in order to obtain a hydroentangled absorbent composite nonwoven.
  • the spunbonded layer (A) that comprises very fine continuous microfilaments (DI ⁇ 15 ⁇ m) and is pre-consolidated with a microbonding pattern having a very high bonding dots density ( ⁇ 90 dots/cm 2 ), advantageously constitutes a good barrier for the pulp fibres during the hydrodynamic needling of the composite, thereby reducing the pulp loss, and enables to achieve good mechanical properties, good uniformity, and good softness for the composite nonwoven.
  • steps (a), (b), (c) and (d) of the method of the invention are advantageously performed continuously on one production line. But within the scope of the invention, some steps of the method can be performed separately on separate production lines.
  • the pre-consolidated spunbonded layer (A) can be produced on a first production line (steps (a) and (b)), and stored in the form of a roll. Then this pre-consolidated spunbonded layer (A) is transported to a second production line, where it can be used for performing the following steps (c) and (d) of the method of the invention.
  • the method of the invention comprises an additional step of providing a nonwoven cover layer (C) onto and in contact with the absorbent pulp layer (B) before the step (d) of consolidating the composite nonwoven
  • the said nonwoven cover (C) can be either produced continuously in line with the other steps on the same production line, or can be produced separately on a first production line, and be transported and used on a second production line where the other steps are performed.
  • pulp layer used therein and in the claims encompass any absorbent layer essentially comprising pulp.
  • Pulp refers to absorbent material made of or containing fibres from natural sources such a as woody and non-woody plants.
  • Woody plants include, for example, deciduous and coniferous trees.
  • Non-woody plants include, for example, cotton, flax, esparto grass, milkweed, straw, jute hemp, and bagasse.
  • the absorbent pulp layer can be made solely of pulp fibres, but can be also be made of a dry mixture of pulp fibres with other materials, provided the said mixture can be dry-laid onto the consolidated spunbonded layer of the invention, by air-laid techniques or the like.
  • the method of the invention further comprises an additional step of providing a nonwoven cover layer (C) onto and in contact with the absorbent pulp layer (B) before the step (d) of consolidating the composite nonwoven. More preferably, this additional step comprises the following sub-steps:
  • the present invention further relates to a novel pre-consolidated spunbonded web defined in independent claim 17, to a novel composite nonwoven defined in independent claim 21, and to a novel hydroentangled absorbent composite nonwoven defined in independent claim 23.
  • the present invention further relates to a novel continuous system defined in independent claim 33, for producing the hydroentangled absorbent composite nonwoven of the invention.
  • the composite nonwoven of the invention can be used advantageously in all applications, where the absorption of liquid is needed.
  • the composite nonwoven of the invention is preferably used, but not only, in the field of hygienic industry, for making absorbent hygienic products.
  • the present invention thus further relates to the use of this novel composite nonwoven for making hygienic products, and more particularly dry wipes, or wet wipes, or diapers, or training pants, or sanitary napkins, or incontinence products.
  • a hydroentangled absorbent composite nonwoven of the invention comprises at least two superposed layers : a pre-consolidated spunbonded web A, and an absorbent pulp layer B, that is adjacent to said pre-consolidated spunbonded web A.
  • the composite nonwoven optionally comprises a nonwoven cover layer C adjacent to the absorbent pulp layer B, said pulp layer B being sandwiched between the spunbonded web A and the nonwoven cover layer C.
  • the composite nonwoven (A/B/C) of figure 1 is, for example, advantageously manufactured by means of the continuous system of figure 2 .
  • the continuous system of figure 2 comprises a spunbonding unit 1, a thermal bonding unit 2, an air-laid unit 3, a carding unit 4, a hydraulic needling unit 5, a dewatering unit 6, a drying unit 7, and a winding unit 8.
  • the spunbonding unit 1 is used for producing a non-consolidated spunbonded web A' made of continuous spun filaments F.
  • the spunbonding unit 1 comprises at least one supplying line S1.
  • Said supplying line S1 comprises a feeding hopper 10, an extruder 11 and metering pumps 12.
  • the feeding hopper 10 contains a polymeric material P (for example in the form of pellets, or chips, or granulates,).
  • Said hopper 10 is connected to the inlet of the extruder 11, that enables to continuously heat up and molten the polymeric material P.
  • the outlet of the extruder 11 is connected to the inlet of metering pumps 12, via a distribution manifold.
  • the outlets of the metering pumps 12 are connected to the inlet of a spinning pack 13.
  • the metering pumps 12 are used for continuously dosing the molten polymer P into the spinning pack 13. This spinning pack 13 is used for producing a curtain of continuous filaments F'.
  • the spunbonding unit 1 further comprises a second supplying line S2 for feeding the spinning pack 13 with a polymeric material P'.
  • This second supplying line S2 comprises a feeding hopper 10', that contains the polymeric material P', an extruder 11', and metering pumps 12'.
  • the spunbonding unit 1 Downstream the spinning pack 13, the spunbonding unit 1 comprises an air quenching box 14 that is being used to cool down the filaments F' issued from the spinning pack 13, and an air drawing equipment 15 that is being used to reduce the diameter of the filaments in order to form a curtain of filaments F having a smaller diameter.
  • the polymeric material(s) [P and/or P'] used for making the continuous spun filaments F can be any known spinnable polymeric material, and for example, polyolefin (in particular polypropylene or polyethylene), polyester, or polyamide, or any biodegradable thermoplastic polymer, like for example polylactic acid (PLA), or any blend thereof, or any copolymers thereof, or any blend of copolymers thereof.
  • polyolefin in particular polypropylene or polyethylene
  • polyester or polyamide
  • any biodegradable thermoplastic polymer like for example polylactic acid (PLA), or any blend thereof, or any copolymers thereof, or any blend of copolymers thereof.
  • These continuous spun filaments F can be, for example, monocomponent or multicomponent filaments, especially bicomponent filaments, and more especially sheath/core bicomponent filaments.
  • monocomponent spun filaments F are produced, only one supplying line (S1 or S2) can be used or both supplying lines can be used (S1 and S2).
  • bicomponent spun filaments F are produced, both supplying lines S1 and S2 are used simultaneously.
  • sheath/core bicomponent filaments it is preferred, but not mandatory, to use polyethylene/polypropylene filaments.
  • the filaments F have a bilobal shape.
  • the shape in cross section of the continuous spun filament F is determined by the geometry of the holes of the spinneret plate of the spinning pack 13.
  • Some non-limiting examples of different cross sections for monocomponent filaments are illustrated on figures 12A, 12B and 12C and some non-limiting examples of different cross sections for bi-component filaments are illustrated on figures 12D, 12E, 12F, 12G, 12H .
  • the bilobal filaments of figure 12C and 12G are suitable for the invention.
  • the air drawing equipment 15 is mounted above a movable and foraminous surface, such as a wire conveyor belt 16.
  • the spun filaments F of reduced diameter, that are issued from the air drawing equipment 15, are laid down onto the said movable surface 16, where vacuum is applied, opposite to the filaments lay down side, by means of a vacuum box 17.
  • a non-consolidated spunbonded web A' made of continuous spun filaments F is thus formed on the surface of the belt 16, and is transported by the belt 16 towards the thermal bonding unit 2, that is mounted downstream the spunbonding unit 1.
  • these continuous spun filaments F are microfilaments having a diameter DI less than or equal to 15 ⁇ m, and more preferably less than 10 ⁇ m.
  • the spunbonded web A' is a light web whose weight is between 7 g/m 2 and 35g/m 2 , preferably less than 25 g/m 2 , more preferably less than 15 g/m 2 , and even more preferably less than 12 g/m 2 .
  • the spunbonding unit 1 is knowingly set up by one skilled in the art, in order to produce such a light spunbonded web A' made of continuous spun filaments F, that comprise or are constituted by very fine spun microfilaments having a diameter DI less than or equal to 15 ⁇ m, and more preferably less than or equal to 10 ⁇ m.
  • the diameter DI of said filament F can be checked as follows.
  • a sample of a filament F is being collected (for example on the belt 16), and the filament count CT is measured by applying the following known gravimetric method: the length of the sample is measured and the sample is being weighted.
  • the weight of the sample expressed in g (grams), is then correlated to the weight of 10000 meters of filament, in order to obtain the filament count (in dtex).
  • the density d of the polymer is well-known in the art.
  • the density of several homopolymer that are suitable for the invention are the following:
  • the diameter DI of the filament can also be measured by using an optical or electronic microscope. In that case, depending on the fiber diameter uniformity, it is recommended to perform several measurements of the filament diameter at different locations along the sample length, and to calculate an average value for the diameter DI.
  • the spunbonded web A' is fed to a thermal bonding unit 2, that is being used in order to pre-consolidate the spunbonded web A' by heat and mechanical compression (thermo-bonding), and form the pre-consolidated spunbonded web A of the composite nonwoven of figure 1 .
  • a thermal bonding unit 2 that is being used in order to pre-consolidate the spunbonded web A' by heat and mechanical compression (thermo-bonding), and form the pre-consolidated spunbonded web A of the composite nonwoven of figure 1 .
  • said thermal bonding unit 2 is a calender that comprises two heated pressure rolls 20, 21.
  • the lower roll has a smooth surface, and is for example a smooth steel roll.
  • the upper roll 21 has an engraved surface with protruding ribs, that are regularly distributed over the whole surface of the roll, and that form a micro-bonding pattern.
  • micro-bonding pattern for roll 21 that is suitable for practicing the invention is shown on figures 5 to 7 .
  • This micro-bonding pattern will be referred hereafter "C#1".
  • the upper surface 210a of each protruding rib 210 forms one bonding dot.
  • the heating temperature of said rolls 20, 21 is set up in order to obtain a softening of the surface of the filaments F.
  • the mechanical pressure exerted by the rolls on the spunbonded web is sufficient in order to obtain a thermo-bonding of the spun filaments F, under heat and pressure.
  • the density of the bonding dots 210a (i.e. the number of bonding dots 210a per cm 2 ) of the upper engraved roll 21 is very high, and at least equal to 90 bonding dots/cm 2 , and more preferably at least equal to 100 bonding dots/cm 2 ; the bonding ratio is low, and preferably less than 30% and more preferably less than 20%.
  • each bonding dot 210a is less than 0.5mm 2 , preferably less than 0.3mm 2 , and more preferably less than 0.2mm 2 .
  • the bonding dots 210a of the bonding pattern "C#1" have the same oval shape and the main dimensions of said bonding pattern are the followings :
  • the invention is however hot limited to this particular bonding pattern of figures 5 to 7 .
  • the bonding dots 210a can have different shapes (round shape, square shape, rectangular shape, etc%), and one bonding pattern can be constituted by a combination of bonding dots 210a of different shapes.
  • Figure 10 shows a photography of an example of a pre-consolidated spunbonded web A of the invention, having a basis weight of 14g/m 2 .
  • This pre-consolidated spunbonded web is made of spun filaments (F) that are made of homopolymer of polypropylene, and that have the so-called "papillon" cross section of figure 12C , and a diameter DI of 12 ⁇ m.
  • This spunbonded web was thermo-bonded with a calendar unit 2, using the aforesaid microbonding pattern C#1.
  • the pre-consolidated spunbonded layer A issued from the thermal bonding unit 2, comprises a high number of very small bonded dots 210b, that corresponds to the bonding pattern of the engraved roll 21, and wherein the spun microfilaments are locally fused at their surface.
  • the density (DD) of these bonded dots 210b is the same than the density of the bonding dots 210a ( ⁇ 90 bonded dots/cm 2 ).
  • the area of each bonded dots 210b of the pre-consolidated spunbonded layer A is preferably equal or less than the area of the corresponding bonding dot 210a of the bonding pattern.
  • the traditional air-laid unit 3, which is mounted downstream the thermal bonding unit 2, is disclosed in details, for example, in European patent application EP 0 032 772 .
  • Said air-laid unit 3 is fed with loose pulp fibers, and more preferably with short wood pulp fibers.
  • the pre-consolidated spunbonded web A issued from thermal bonding unit 2 is transferred continuously to a second belt 30 where pulp fibers are laid down, using a conventional air-laid process, by means of said traditional air-laid unit 3.
  • the air-laid unit 3 is set up in order to produce a pulp layer B whose weight is between 15 g/m 2 and 50 g/m 2 .
  • a composite (A/B) made of a pre-consolidated spunbonded web A and of an absorbent pulp top layer B is obtained.
  • the carding unit 4 which is mounted between the air-laid unit 3 and the hydraulic needling unit 5, is used for producing in line a carded nonwoven cover layer C. Said carded nonwoven cover layer C issued from the carding unit 4 is laid down onto the top surface of the absorbent pulp layer B of the composite nonwoven (A/B) issued from the air-laid unit 3.
  • the carding unit 4 is set up in order to produce a carded layer C, whose weight is between 10 g/m 2 and 30 g/m 2 .
  • the composite nonwoven (A/B/C) is transported, downstream the carding unit 3, by means of a third conveyor belt 50 through the hydraulic needling unit 5.
  • This hydraulic needling unit 5 is used for consolidating the nonwoven composite (A/B/C), by means of high pressure water jets (hydroentanglement process) that are directed at least towards the surface of the top layer (cover layer C), and that penetrate through the structure of the composite and are partially reflected back to the structure, in order to bind the layers (A, B and C) together.
  • the water needling process is performed on both sides of the composite nonwoven (A/B/C).
  • the hydraulic needling unit 5 comprises four successive perforated drums.
  • First perforated drum 51 is associated with two successive hydro-jet beams 51 a and 51 b.
  • Second perforated drum 52 is associated with two successive hydro-jet beams 52a and 52b.
  • Third perforated drum 53 is associated with two successive hydro-jet beams 53a and 53b.
  • Fourth perforated drum 54 is associated with two successive hydro-jet beams 54a and 54b.
  • the water pressure of the upstream hydro-jet beam 51a is lower than the water pressure of all the other downstream hydro-jet beams 51 b, 52a, 52b, 53a, 53b, 54a, 54b, in order to obtain a pre-hydroentanglement of the layers.
  • This hydroentangled and absorbent composite A/B/C is transported downstream the hydraulic needling unit 5 by the conveyor belt 60 of a dewatering unit 6, and over a vacuum box 61, that enables to remove by suction from the composite A/B/C most of the water that has been absorbed during the water needling process (conventional dewatering process).
  • the hydroentanglement unit 5 and the dewatering unit 6 can be integrated in the same industrial equipment.
  • the dewatered hydroentangled absorbent composite nonwoven A/B/C issued from the dewatering unit 6 is continuously fed through the oven of the drying unit 7, wherein heat is applied to the composite (for example by means of hot air), in order to remove the remaining water still contained within the composite nonwoven.
  • the dried composite nonwoven A/B/C is wound in the form of a roll, by means of the winding unit 8.
  • the weight of said hydroentangled and absorbent composite A/B/C is between 27 g/m 2 and 115 g/m 2 .
  • Examples N° 1 to N°18 of a pre-consolidated spunbonded web A were produced with the spunbonding unit 1 and thermal bonding unit 2 of figures 2 or 3 .
  • the main production data for each sample N°1 to 18 are summarized hereafter in tables 1A, 1B and 1C.
  • Table 1A Spunbonded production data - Spinning RAW MATERIALS FILAMENT SPINNING [Filaments F'- Spunbonding unit (1)] Ex Polymer(s) type(s) Polymer(s) percentage(s) Spinneret type (holes per meter / hole diameter) filaments section shape filaments diameter DI filaments count CT (dtex) Through put (ghm) N° _ [%] [holes per m / mm] _ [ ⁇ m] [g/10000m] [g/hole/ min] 1 PP (1) 100 5000 / 0.35 round 9.5 0.65 0.33 2 PP (1) 100 5000 / 0.35 round 12.4 1.10 0.33 3 PP (1) 100 5000 / 0.35 round 13.5 1.30 0.33 4 PP (1) 100 5000 / 0.35 round 17.1 2.10 0.33 5 PP (2) 100 6000 / 0.35 round 9.7 0.67 0.29 6 PP (2) 100 6000 / 0.35 round 12.3 1.08 0.29 7 PP (2) 100 6000 / 0. 0.
  • the filaments of the spunbonded web were round monocomponent filaments made of homopolymer of polypropylene.
  • the filaments of the spunbonded web were bilobal monocomponent filaments made of homopolymer of polypropylene.
  • the bilobal shape of the filaments (also called "papillon") is well-known and shown on figure 12C .
  • the weight of the spunbonded web was around 10 g/m 2 ;
  • the weight of the spunbonded web was around 32 g/m 2 .
  • the weight of the spunbonded web was around 13g/m 2 .
  • Examples N°5 to N°7 (10 g/m 2 ) and examples N° 12 and N°13 (32 g/m 2 ) relate to pre-consolidated spunbonded webs, which have been compressed and thermo-bonded with the same engraved roll 21 having the previously described micro-bonding pattern "C#1". They differ from each other by the diameter (DI) of their continuous spun microfilaments (F).
  • Examples N°1 to N°4 (10 g/m 2 ) and examples N°9 to N°11 (32 g/m 2 ) relate to spunbonded webs which have been compressed and thermo-bonded with the same engraved roll 21, said engraved roll 21 having the bonding pattern of figures 8 and 9 .
  • the main dimensions of this bonding pattern (referred therein "C#2") were the followings :
  • Example N°8 (10 g/m 2 ) and example N°14 (32 g/m 2 ) relate to pre-consolidated spunbonded webs, which have been thermo-bonded with microbonding pattern "C#1", but which are made of continuous spun filaments (F), having a diameter (DI) higher than 15 ⁇ m (i.e. outside the scope of the invention).
  • the air permeability of the pre-consolidated spunbonded web was measured according to the following method.
  • Air Permeability Test was performed on a Textest model FX 3300 available from the Textest Instruments - Zurich, according to WSP 70.1 (05) standard. The rate of air flow passing perpendicularly through a given area of fabric is measured at a given pressure difference across the fabric test area over a given time period.
  • the specimen (a single layer) was positioned in the circular specimen holder, with an orifice allowing the test to be carried out on an area of 38cm 2 .
  • the pressure gap was set at 125 Pa.
  • Table 2A Spunbonded web -10 g/m 2 - Air permeability versus spun filament diameter NONWOVEN Air Permeability Ref.
  • the air permeability measurements show that the air permeability of the pre-consolidated spunbonded web A increases with the spun filament diameter (DI) and decreases with the density (DD) of the bonding dots.
  • Pre-consolidated spunbonded webs of Examples N°5, N°6, N°7, N°12 and N°13 advantageously exhibit lower air permeability, and the spunbonded layer constitutes therefore an improved barrier for the pulp fibres during the water needling process of the composite nonwoven.
  • Example N° 19 to N°26 of a three-layered hydroentangled and absorbent composite nonwoven (A/B/C) were produced by means of a continuous system like the one previously described and shown on figure 2 .
  • the main production data for these examples N°19 to 26 are summarized hereafter in tables 4A, 4B and 4C.
  • Table 4A Composite nonwoven A/B/C (Spun/Pulp/Carded)-Production data RAW MATERIALS SPC Basis Weight (A/B/C) SPUNBONDED (A) PULP (B) CARDED (C) Ex Total A B C Spunbonded type Pulp type Fibre(s)type(s) N° [g/m 2 ] [g/m 2 ] [g/m 2 ] [g/m 2 ] [g/m 2 ] Ex _ _ 19 45 10 22 13 N°2 (I) (II) 20 45 10 22 13 N°1 (I) (II) 21 45 10 22 13 N°5 (I) (II) 22 45 10 22 13 N°6 (I) (II) 23 90 32 33 25 N°10 (I) (III) 24 90 32 33 25 N°9 (I) (III) 25 90 32 33 25 N°13 (I) (III) 26 90 32 33 25 N12 (I) (III) (I) Weyerhauser, NF 405
  • the basis weight of the composite nonwoven of examples N°19 to 22 was 45 g/m 2 .
  • the basis weight of the composite nonwoven of examples N°23 to 26 was 90 g/m 2 .
  • Examples N°19, N°20, N°23 and N°24 relate to hydroentangled and absorbent composite nonwoven comprising a spunbonded layer A that is the same respectively than examples N°2, N°1, N°10 and N°9.
  • Examples N°21, N°22, N°25 and N°26 relate to hydroentangled and absorbent composite nonwoven comprising a spunbonded layer A that is the same respectively than examples N°5, N°6, N'13 and N°12.
  • Table 4B Composite nonwoven A/B/C (Spun/Pulp/Carded)-Hydroentanglement step HYDROENTAGLEMENT (UNIT 5) Ex.
  • Abrasion resistance testing was performed on a Martindale Abrasion Tester (Model: Nu-Martindale Abrasion and Pilling tester from James H. Heal & Co. Ltd - Suite, England). Tests were performed according to ASTM D 4966-98 using a pressure of 12 kilopascals (KPa) on the spunbonded side (A) of the composite A/B/C.
  • KPa kilopascals
  • Samples were subjected to 150 cycles and were then examined for the presence of surface fuzzing, pilling, roping or holes.
  • the samples were compared to a visual scale and assigned a wear number from 1 to 5, wherein wear number 5 was indicating little or no visible abrasion and wear number 1 was indicating a hole worn through the sample.
  • Table 5A Composite SPC - 45 g/m 2 - Abrasion resistance SPC (A/B/C) SPUNBONDED (A) MARTINDALE ABRASION Ref. Method: ASTM D4966-98 Ex.
  • the pre-consolidated spunbonded layers A of examples N°21, 22, 25 and 26 have advantageously a better abrasion resistance than the pre-consolidated spunbonded layers of the other comparative examples.
  • the comparison between examples having the same basis weight and having spun filaments of similar diameter (Ex. N°19 vs. Ex. N°23; EX. N°20 vs. Ex. N°21 ; EX. N°23 vs. Ex. N°25 ; EX. N°24 vs. Ex. N°26) further shows that the microbonding pattern of the invention, with very high density of bonding dots (DD), improves the abrasion resistance of the spunbonded layer A, compared with the use of a bonding pattern having a low density of bonding dots (DD).
  • DD very high density of bonding dots
  • Handle-O-Meter testing was performed on a Handle-O-Meter Model no. 211-5, model 211-2001 available from the Thwing-Albert Company. Tests were performed according to WSP 90.3.0 (05) standard. The nonwoven to be tested is deformed through a restricted opening by a plunger and the required force corresponds to the surface friction of the nonwoven.
  • the results of the handle-o-meter test are summarized hereafter in table 6A (basis weight 45 g/m 2 ) and in table 6B (basis weight 90 g/m 2 ).
  • the composite nonwovens (A/B/C) of examples N°21, 22, 25 and 26 have advantageously a lower stiffness both in CD and MD directions (and thus a higher softness) than the other comparative examples.
  • the comparison between examples having the same basis weight and having spun filaments of similar diameter (Ex. N°19 vs. Ex. N°22; EX. N°20 vs. Ex. N°21 ; EX. N°23 vs. Ex. N°25 ; EX. N°24 vs. Ex.
  • N°26 shows that the microbonding pattern of the invention, with very high density of bonding dots (DD), improves the softness of the final product, compared with the use of a bonding pattern having a low density of bonding dots (DD).
  • Table 6A Composite SPC - 45 g/m 2 - stiffness (handle-o-meter test) SPC (A/B/C) HANDLE-O-METER Ref.
  • Tensile strength refers to the maximum load (i.e., peak load) encountered while elongating the sample to break. Elongation at peak is the specimen elongation that corresponds to the peak load. Measurements were made in cross-direction on dry samples.
  • Specimens were cut 25mm width and 125mm length. The distance between the clamps of the dynamometer was set at 75mm and the traction speed was set at 300mm/min.
  • Table 7A Composite SPC - 45 g/m 2 - Tensile properties (MD, CD) SPC(A/B/C) SPUNBONDED TENSILE PROPERTIES Ref.
  • figure 11 shows a photography of a sample of a hydroentangled absorbent composite nonwoven (A/B/C), having a basis weight of 50 g/m 2 , and wherein:
  • the spunbonded layer A was thermo-bonded with a calendar unit 2, using the aforesaid microbonding pattern C#1.This photography was taken on the spunbonded side (A) of the composite nonwoven. This composite nonwoven exhibits a high uniformity.
  • the invention is not limited to hydroentangled composite made of three layers (A/B/C), but the absorbent composite nonwoven could be made solely of the two layers A and B.
  • the cover layer C is not necessarily a carded layer, but can be any other nonwoven layer, and in particular a spunbonded layer.
  • the carding unit 4 of figure 2 has been replaced by a second spunbonding unit 1'.
  • the cover layer C of the composite nonwoven is not a carded layer, but is replaced by a spunbonded layer made of continuous filaments.
  • the spunbonded layer C can be made of spun microfilaments having a diameter DI less or equal than 15 ⁇ m, or can be made of thicker spun filaments.
  • Figure 4 shows another continuous system of the invention for producing a hydroentangled and absorbent composite nonwoven made of three layers.
  • the carding unit 4 of figure 2 has been replaced by a second spunbonding unit 1' and by a thermal bonding unit 2' that are similar to the previously described spunbonding unit 1 and thermal bonding unit 2.
  • the thermal bonding unit 2' comprises two heated rolls 20' and 21'.
  • the lower roll 20' has a smooth surface, and is for example a smooth steel roll.
  • the upper roll 21' has an engraved surface with protruding ribs, that are regularly distributed over the whole surface of the roll, and that form a bonding pattern having bonding dots 210a (like roll 21 of thermal bonding unit 2).
  • the continuous system of figure 4 is used for producing a hydroentangled and absorbent composite nonwoven made of three layers: a carrier layer constituted by the pre-consolidated spunbonded layer (A) previously described for the embodiment of figure 2 ; an intermediate pulp layer (B) previously described for the embodiment of figure 2 ; a cover layer (C) constituted by a pre-consolidated spunbonded layer.
  • the said second spunbonding unit 1' is set up in order to produce a spunbonded web C' made of spun filaments that comprise or are constituted by very fine spun microfilaments having a diameter DI less than or equal to 15 ⁇ m, and more preferably less than or equal to 10 ⁇ m. More preferably, the spunbonded web C' is a web whose weight is between 7 g/m 2 and 35g/m 2 , preferably less than 25 g/m 2 , more preferably less than 12 g/m 2 .
  • the density DD of the bonding dots 210a of the engraved roll 21' is also very high, and at least equal to 90 bonding dots/cm 2 , and more preferably at least equal to 100 bonding dots/cm 2 ; the bonding ratio (R) is low, and preferably less than 30% and more preferably less than 20%.
  • the area DA of each bonding dot 210a of engraved roll 21' is less than 0.5mm 2 , preferably less than 0.3mm 2 , and more preferably less than 0.2mm 2 .
  • Different shapes for bonding dots 210a of the engraved roll 21' are suitable for practicing the invention (round shape, oval shape, square shape, rectangular shape ).
  • the microbonding pattern of the engraved roll 21' can be the same as the microbonding pattern of the engraved roll 21 of thermal bonding unit 2, but this is not mandatory.
  • the composite nonwoven (A/B/C) produced with the aforesaid preferred embodiment of continuous system of figure 4 has advantageously comparable properties on both sides of the composite nonwoven.
  • the composite of the invention can comprise more than three superposed layers.
  • an additional layer for example a carded layer
  • this additional layer is for example laid onto conveyor belt 16, upstream the spunbonding unit 1, and the continuous spun filaments F are laid directly onto this additional layer.
  • the invention is not limited to the use of the pre-consolidated spunbonded web (A) of the invention for making the hydroentangled absorbent composite nonwovens (A/B) or (A/B/C) previously described in detailed in reference to the attached drawings.
  • the pre-consolidated spunbonded web (A) of the invention can be used alone or can be used as a layer of any known types of composite nonwovens comprising at least two superposed layers.
  • the composite nonwovens comprising the pre-consolidated spunbonded web (A) of the invention can be consolidated by any know bonding means, including notably thermal bonding, adhesive bonding, mechanical needling, hydrodynamic needling.
  • the pre-consolidated spunbonded web (A) of the invention can be used advantageously for making a hydroentangled spunbonded/carded nonwoven.
  • figure 13 shows a photography of a sample of a hydroentangled composite nonwoven (A/C), having a basis weight of 45 g/m 2 , and wherein:
  • Said hydroentangled spunbonded/carded nonwoven can be advantageously used for making the top sheets of diapers or training pants.
  • Said hydroentangled spunbonded/carded nonwoven can be manufactured with a production line according to the one depicted on figure 2 , but without the air-laying unit 3 or without using the air-laying unit 3.

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  • Engineering & Computer Science (AREA)
  • Textile Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Nonwoven Fabrics (AREA)
  • Yarns And Mechanical Finishing Of Yarns Or Ropes (AREA)
  • Laminated Bodies (AREA)

Claims (39)

  1. Procédé de fabrication d'un tissu spunbonded pré-consolidé (A), ledit procédé comprenant les étapes consistant à :
    (a) former une couche spunbonded (A'),
    (b) thermolier ladite couche spunbonded (A') afin d'obtenir un tissu spunbonded préconsolidé (A),
    caractérisé en ce que la couche spunbonded (A') formée à l'étape (a) comprend des microfilaments continus bilobés ayant un diamètre (DI) inférieur ou égal 15 µm, et en ce que l'étape de préconsolidation (b) de la couche spunbonded (A') est effectuée au moyen d'un motif de liage ayant des points de liage (210a), la densité (DD) desdits points de liage (210a) étant supérieure ou égale à 90 points/cm2.
  2. Procédé selon la revendication 1, caractérisé en ce que l'étape de préconsolidation (b) de la couche spunbonded (A') est effectuée avec un motif de liage ayant un faible taux de liage (R) inférieur à 30 %.
  3. Procédé selon les revendications 1 ou 2, caractérisé en ce que l'étape de préconsolidation (b) de la couche spunbonded (A') est effectuée avec un motif de liage comprenant des points de liage (210a) ayant une surface de liage inférieure à 0,5 mm2.
  4. Procédé de fabrication selon l'une quelconque des revendications 1 à 3, caractérisé en ce que le poids de la couche spunbonded (A') n'excède pas 15 g/m2, et plus préférablement n'excède pas 12 g/m2.
  5. Procédé de fabrication d'un non-tissé composite hydroenchevêtré comprenant au moins deux couches superposées, caractérisé en ce qu'il comprend les étapes suivantes :
    - la formation d'une couche spunbonded préconsolidée (A) selon l'une quelconque des revendications 1 à 4,
    - le dépôt d'au moins une seconde couche (B) sur ladite couche spunbonded préconsolidée (A),
    - la consolidation des couches par aiguilletage hydrodynamique.
  6. Procédé selon la revendication 5, caractérisé en ce que la seconde couche est une couche cardée ou une couche spunbonded.
  7. Procédé selon la revendication 5 pour fabriquer un non-tissé composite absorbant hydroenchevêtré, caractérisé en ce que la seconde couche est une couche de pâte.
  8. Procédé selon l'une quelconque des revendications 5 à 7, caractérisé en ce qu'il comprend en outre une étape supplémentaire de fourniture d'une couche de recouvrement de non-tissé (C) sur et en contact avec la seconde couche (B) avant l'étape de consolidation du non-tissé composite par aiguilletage hydrodynamique.
  9. Procédé selon la revendication 8, caractérisé en ce que la couche de recouvrement de non-tissé (C) est une couche cardée ou une couche spunbonded.
  10. Procédé selon la revendication 9, caractérisé en ce que l'étape supplémentaire de fourniture d'une couche de recouvrement de non-tissé (C) comprend les sous-étapes suivantes :
    (a') la formation d'une couche spunbonded (C')
    (b') le thermoliage de ladite couche spunbonded (C') afin d'obtenir une couche spunbonded préconsolidée (C).
  11. Procédé selon la revendication 10, caractérisé en ce que la couche spunbonded (C') formée dans la sous-étape (a') comprend des microfilaments continus ayant un diamètre (DI) inférieur ou égal à 15 µm, et en ce que la sous-étape de préconsolidation (b') de la couche spunbonded (C') est effectuée au moyen d'un motif de liage ayant des points de liage (210a), et ayant les caractéristiques techniques définies dans l'une quelconque des revendications 1 à 3 pour le motif de liage utilisé pour fabriquer la couche spunbonded préconsolidée (A).
  12. Procédé selon l'une quelconque des revendications 8 à 11, caractérisé en ce que le poids de la couche de recouvrement (C) est inférieur à 30 g/m2.
  13. Procédé selon l'une quelconque des revendications 10 à 12, caractérisé en ce que le poids de la couche spunbonded (A') est inférieur à 35 g/m2, de préférence inférieur à 25 g/m2, plus préférablement inférieur à 15 g/m2, et encore plus préférablement inférieur à 12 g/m2.
  14. Procédé selon l'une quelconque des revendications 7 à 13, caractérisé en ce que le poids de la couche de pâte (B) est inférieur à 50 g/m2.
  15. Procédé selon l'une quelconque des revendications 7 à 14, caractérisé en ce que le poids du non-tissé composite est inférieur à 115 g/m2.
  16. Procédé selon l'une quelconque des revendications 8 à 15, caractérisé en ce que le poids du non-tissé composite (A/B/C) est compris entre 27 g/m2 et 115g/m2, en ce que le poids de la couche de support spunbonded préconsolidée (A) est compris entre 7 g/m2 et 35 g/m2, en ce que le poids de la couche de pâte (B) est compris entre 10 g/m2 et 50 g/m2, et en ce que le poids de la couche de recouvrement (C) est compris entre 10 g/m2 et 30 g/m2.
  17. Tissu spunbonded préconsolidé (A), caractérisé en ce qu'il comprend des microfilaments continus bilobés ayant un diamètre (DI) inférieur ou égal à 15 µm, et des points liés (210b), la densité (DD) desdits points liés (210b) étant supérieure ou égale à 90 points/cm2.
  18. Tissu spunbonded préconsolidé selon la revendication 17, caractérisé par un taux de liage (R') qui est inférieur à 30 %.
  19. Tissu spunbonded préconsolidée selon la revendication 17 ou 18, caractérisé en ce que les points liés (210b) ont une surface inférieure à 0,5 mm2.
  20. Tissu spunbonded préconsolidé selon l'une quelconque des revendications 17 à 19, ayant une masse surfacique n'excédant pas 15 g/m2, et de préférence n'excédant pas 12 g/m2.
  21. Non-tissé composite comprenant au moins une première et une seconde couche, caractérisé en ce que la première couche est un tissu spunbonded préconsolidé selon l'une quelconque des revendications 17 à 20.
  22. Non-tissé composite selon la revendication 21, caractérisé en ce que la seconde couche est une couche cardée, ou une couche de pâte, ou une couche spunbonded.
  23. Non-tissé composite hydroenchevêtré absorbant comprenant une couche spunbonded préconsolidée (A) selon l'une quelconque des revendications 17 à 22 et une couche de pâte absorbante (B) en contact avec la couche spunbonded préconsolidée (A).
  24. Non-tissé composite selon la revendication 23, caractérisé en ce qu'il comprend en outre une couche de recouvrement de non-tissé supplémentaire (C) en contact avec la couche de pâte absorbante (B).
  25. Non-tissé composite selon la revendication 24, caractérisé en ce que la couche de recouvrement de non-tissé (C) est une couche cardée ou une couche spunbonded.
  26. Non-tissé composite selon la revendication 25, caractérisé en ce que la couche de recouvrement de non-tissé (C) est un tissu spunbonded préconsolidé selon l'une quelconque des revendications 17 à 20.
  27. Non-tissé composite selon l'une quelconque des revendications 23 à 26, caractérisé en ce que le poids de la couche de recouvrement (C) est inférieur à 30 g/m2.
  28. Non-tissé composite selon l'une quelconque des revendications 23 à 27, caractérisé en ce que le poids de la couche spunbonded préconsolidée (A) est inférieur à 35 g/m2, de préférence inférieur à 25 g/m2, plus préférablement inférieur à 15 g/m2 et encore plus préférablement inférieur à 12 g/m2.
  29. Non-tissé composite selon l'une quelconque des revendications 23 à 28, caractérisé en ce que le poids de la couche de pâte (B) est inférieur à 50 g/m2.
  30. Non-tissé composite selon l'une quelconque des revendications 23 à 29, caractérisé en ce que le poids du non-tissé composite est inférieur à 115 g/m2.
  31. Non-tissé composite selon l'une quelconque des revendications 24 à 30, caractérisé en ce que le poids du non-tissé composite (A/B/C) est compris entre 27 g/m2 et 115 g/m2, en ce que le poids de la couche spunbonded préconsolidée
    (A) est compris entre 7 g/m2 et 35 g/m2, en ce que le poids de la couche de pâte
    (B) est compris entre 10 g/m2 et 50 g/m2, et en ce que le poids de la couche de recouvrement (C) est compris entre 10 g/m2 et 30 g/m2.
  32. Utilisation du non-tissé composite selon l'une quelconque des revendications 23 à 31, pour fabriquer des produits hygiéniques, et plus particulièrement des lingettes sèches, ou des lingettes humides, ou des couches, ou des culottes de propreté, ou des serviettes hygiéniques ou des produits pour l'incontinence.
  33. Système continu pour fabriquer un non-tissé composite absorbant hydroenchevêtré selon l'une quelconque des revendications 23 à 32, caractérisé en ce qu'il comprend :
    - une unité de spunbond (1) pour fabriquer une couche spunbonded (A') comprenant des microfilaments continus bilobés ayant un diamètre (DI) inférieur ou égal à 15 µm,
    - unité de thermoliage (2) montée en aval de l'unité de spunbond (1) et comprenant un rouleau gravé (21) ayant un motif de liage caractérisé par une densité de points de liage (DD) qui est supérieure ou égale à 90 points/cm2,
    - une unité d'arrangement par flux d'air (3), montée en aval de l'unité de spunbond (1), et alimentée avec de la pâte,
    - une unité d'aiguilletage hydraulique (5) montée en aval de l'unité d'arrangement par flux d'air (3).
  34. Système continu selon la revendication 33, caractérisé en ce que le taux de liage (R) du motif de liage du rouleau gravé (21) est inférieur à 30 %.
  35. Système continu selon les revendications 33 ou 34, caractérisé en ce que le motif de liage du rouleau gravé (21) comprend des points de liage (210a) ayant une surface inférieure à 0,5 mm2.
  36. Système continu selon l'une quelconque des revendications 33 à 35, caractérisé en ce qu'il comprend en outre une unité de cardage (4) en amont de l'unité d'aiguilletage hydraulique (5).
  37. Système continu selon l'une quelconque de revendications 33 à 36, caractérisé en ce qu'il comprend en outre une unité de spunbond supplémentaire (1) en amont de l'unité d'aiguilletage hydraulique (5).
  38. Système continu selon la revendication 37, caractérisé en ce que l'unité de spunbond supplémentaire (1') est configurée afin de produire une couche spunbonded (C') comprenant des microfilaments continus ayant un diamètre (DI) inférieur ou égal à 15 µm, et de préférence inférieur ou égal à 10 µm.
  39. Système continu selon la revendication 38, caractérisé en ce qu'il comprend une unité de thermoliage supplémentaire (2') qui est montée en aval de l'unité de spunbond supplémentaire (1') et qui comprend un rouleau gravé (21'), et en ce que ledit rouleau gravé (21') a un motif de liage ayant les caractéristiques techniques définies dans l'une quelconque des revendications 33 à 35, pour le rouleau gravé (21) de l'autre unité de thermoliage (2).
EP08715834.1A 2007-02-22 2008-02-18 Nappe de spunbond pré-consolidé, composite non tissé comprenant cette nappe, procédé et système continu de production de ce composite Active EP2113042B2 (fr)

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Applications Claiming Priority (3)

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EP20070003643 EP1961849A1 (fr) 2007-02-22 2007-02-22 Nappe de spunbond pré-consolidé, composite non tissé comprenant cette nappe, procédé et système continu de production de ce composite
EP08715834.1A EP2113042B2 (fr) 2007-02-22 2008-02-18 Nappe de spunbond pré-consolidé, composite non tissé comprenant cette nappe, procédé et système continu de production de ce composite
PCT/EP2008/001236 WO2008101651A1 (fr) 2007-02-22 2008-02-18 Tissu spunbonded pre-consolidé, non tissé composite comprenant ledit tissé spunbonded pre-consolidé, procédé et système continu de production dudit composite

Publications (3)

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EP2113042A1 EP2113042A1 (fr) 2009-11-04
EP2113042B1 EP2113042B1 (fr) 2010-05-26
EP2113042B2 true EP2113042B2 (fr) 2014-10-29

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EP20070003643 Withdrawn EP1961849A1 (fr) 2007-02-22 2007-02-22 Nappe de spunbond pré-consolidé, composite non tissé comprenant cette nappe, procédé et système continu de production de ce composite
EP08715834.1A Active EP2113042B2 (fr) 2007-02-22 2008-02-18 Nappe de spunbond pré-consolidé, composite non tissé comprenant cette nappe, procédé et système continu de production de ce composite

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EP20070003643 Withdrawn EP1961849A1 (fr) 2007-02-22 2007-02-22 Nappe de spunbond pré-consolidé, composite non tissé comprenant cette nappe, procédé et système continu de production de ce composite

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US (1) US20100324515A1 (fr)
EP (2) EP1961849A1 (fr)
AT (1) ATE469257T1 (fr)
CA (1) CA2711623A1 (fr)
DE (1) DE602008001373D1 (fr)
IL (1) IL200494A (fr)
WO (1) WO2008101651A1 (fr)

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CN102211426B (zh) * 2010-04-06 2015-03-25 Jnc株式会社 使用伸长性无纺布的复合体
CN102493129A (zh) * 2011-11-14 2012-06-13 成都彩虹环保科技有限公司 多组分纤维的无纺布制造装置
CN102505346A (zh) * 2011-11-14 2012-06-20 成都彩虹环保科技有限公司 多组分复合纤维的无纺布制造装置
CN103147233B (zh) * 2013-03-18 2015-02-25 浙江金三发非织造布有限公司 纺丝成网浆粕气流成网水刺固结非织造布的生产工艺
CN103147228B (zh) * 2013-03-18 2015-04-29 浙江金三发非织造布有限公司 纺丝成网木浆纸水刺复合非织造布的生产工艺
CN103132249B (zh) * 2013-03-18 2015-04-15 浙江金三发非织造布有限公司 一种浆粕气流成网纺粘复合非织造布及其生产工艺
CN105452553B (zh) * 2013-07-04 2018-09-25 福伊特专利有限公司 用于制造无纺布的方法和设备
BR112017004655B1 (pt) * 2014-09-29 2021-12-07 Kimberly-Clark Worldwide, Inc Artigo absorvente com um sistema absorvente possuindo uma abertura anular
EP3210584A1 (fr) * 2016-02-29 2017-08-30 Fitesa Germany GmbH Étoffe non tissée et son procédé de formation
US10767296B2 (en) * 2016-12-14 2020-09-08 Pfnonwovens Llc Multi-denier hydraulically treated nonwoven fabrics and method of making the same
BR112019012225B1 (pt) * 2016-12-14 2023-02-14 Pfnonwovens Llc Laminado não-tecido e método de fabricação de um laminado nãotecido
CN111556909B (zh) 2017-11-22 2024-04-09 挤压集团公司 熔喷模头尖端组件和方法
US11136699B2 (en) * 2018-05-14 2021-10-05 Fitesa Simpsonville, Inc. Composite sheet material, system, and method of preparing same

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Also Published As

Publication number Publication date
IL200494A0 (en) 2010-04-29
EP2113042A1 (fr) 2009-11-04
WO2008101651A1 (fr) 2008-08-28
EP1961849A1 (fr) 2008-08-27
US20100324515A1 (en) 2010-12-23
ATE469257T1 (de) 2010-06-15
EP2113042B1 (fr) 2010-05-26
CA2711623A1 (fr) 2008-08-28
IL200494A (en) 2012-08-30
DE602008001373D1 (de) 2010-07-08

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